EP1413767A2 - Assemblage de roue de compresseur - Google Patents

Assemblage de roue de compresseur Download PDF

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Publication number
EP1413767A2
EP1413767A2 EP03256589A EP03256589A EP1413767A2 EP 1413767 A2 EP1413767 A2 EP 1413767A2 EP 03256589 A EP03256589 A EP 03256589A EP 03256589 A EP03256589 A EP 03256589A EP 1413767 A2 EP1413767 A2 EP 1413767A2
Authority
EP
European Patent Office
Prior art keywords
compressor wheel
shaft
bore
wheel
compressor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP03256589A
Other languages
German (de)
English (en)
Other versions
EP1413767A3 (fr
Inventor
Anthony Holset Engineering Co. Ltd. Billington
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Cummins Turbo Technologies Ltd
Original Assignee
Holset Engineering Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Holset Engineering Co Ltd filed Critical Holset Engineering Co Ltd
Publication of EP1413767A2 publication Critical patent/EP1413767A2/fr
Publication of EP1413767A3 publication Critical patent/EP1413767A3/fr
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/266—Rotors specially for elastic fluids mounting compressor rotors on shafts

Definitions

  • This invention relates to the assembly of a compressor wheel to a rotating shaft.
  • the invention relates to the compressor wheel assembly of a turbocharger.
  • Turbochargers are well known devices for supplying air to the intake of an internal combustion engine at pressures above atmospheric (boost pressures).
  • a conventional turbocharger essentially comprises an exhaust gas driven turbine wheel mounted on a rotatable shaft within a turbine housing. Rotation of the turbine wheel rotates a compressor wheel mounted on the other end of the shaft within a compressor housing. The compressor wheel delivers compressed air to the intake manifold of the engine, thereby increasing engine power.
  • the shaft is supported on journal and thrust bearings located within a central bearing housing connected between the turbine and compressor wheel housings.
  • a conventional compressor wheel comprises an array of blades extending from a central hub provided with a bore for receiving one end of the turbocharger shaft.
  • the compressor wheel is secured to the shaft by a nut which threads onto the end of the shaft where it extends through the wheel bore, and bears against the nose end of the wheel to clamp the wheel against a shaft shoulder (or other radially extending abutment that rotates with the shaft).
  • a compressor wheel assembly comprising a compressor wheel mounted to a rotating shaft, the shaft extending through a bore provided along the rotational axis of the wheel, wherein the bore has an inner diameter greater than the outer diameter of the portion of the shaft which passes through the compressor wheel, and a cylindrical sleeve is located concentrically around the shaft between the inner surface of the bore and the outer surface of the shaft to thereby support the shaft co-axially within the bore.
  • the present invention enables the shaft bore to be machined with a diameter suitable for accurate mass production, the bore diameter then effectively being reduced to suite the shaft diameter by provision of said sleeve. The manufacturing difficulties of the prior art are therefore avoided.
  • the sleeve may be pre-fitted to the compressor wheel.
  • the present invention also provides a compressor wheel for a turbocharger, which in use is mounted to one end of a turbocharger shaft, wherein the compressor wheel defines an internal axial through bore of a relatively large diameter, and is provided with a cylindrical sleeve of a relatively small inner diameter, selected to correspond to the diameter of the shaft, located co-axially within said bore.
  • FIG. 1 illustrates the basic components of a conventional centripetal type turbocharger.
  • the turbocharger comprises a turbine 1 joined to a compressor 2 via a central bearing housing 3.
  • the turbine 1 comprises a turbine housing 4 which houses a turbine wheel 5.
  • the compressor 2 comprises a compressor housing 6 which houses a compressor wheel 7.
  • the turbine wheel 5 and compressor wheel 7 are mounted on opposite ends of a common shaft 8 which is supported on bearing assemblies 9 within the bearing housing 3.
  • the turbine housing 4 is provided with an exhaust gas inlet 10 and an exhaust gas outlet 11.
  • the inlet 10 directs incoming exhaust gas to an annular inlet chamber 12 surrounding the turbine wheel 5.
  • the exhaust gas flows through the turbine and into the outlet 11 via a circular outlet opening which is co-axial with the turbine wheel 5.
  • Rotation of the turbine wheel 5 rotates the compressor wheel 7 which draws in air through axial inlet 13 and delivers compressed air to the engine intake via an annular outlet volute 14.
  • the compressor wheel comprises a plurality of blades 15 extending from a central hub 16 which is provided with a through bore to receive one end of the shaft 8.
  • the shaft 8 extends slightly from the nose of the compressor wheel 7 and is threaded to receive a nut 17 which bears against the compressor wheel nose to clamp the compressor wheel 7 against a thrust bearing and oil seal assembly 18.
  • Details of the thrust bearing/oil seal assembly may vary and are not important to understanding of the compressor wheel mounting arrangement. Essentially, the compressor wheel 7 is prevented from slipping on the shaft 8 by the clamping force applied by the nut 17.
  • Figure 2 illustrates a compressor wheel assembly in accordance with the present invention. Details of the shaft 8, thrust bearing and seal assembly 18, and clamp nut 17 may be entirely conventional, as for instance illustrated in Figure 1.
  • the compressor wheel bore 21 has a relatively large diameter (i.e. larger than the diameter of the shaft 8) and in particular is of a size that can be easily machined and mass produced to the required accuracy.
  • the diameter of the bore 21 is then effectively reduced to the diameter of the shaft 8 by introduction of a cylindrical sleeve 22 in to the bore 21.
  • the sleeve 22 has an outer diameter corresponding to the inner diameter of the bore 21, and an inner diameter corresponding to the outer diameter of the shaft 8. The shaft 8 is therefore accurately located and maintained along the axis of the bore 21.
  • the sleeve 21 is provided slightly shorter than the length of the bore 20 to ensure that the clamping force is transferred through the compressor wheel and not through the sleeve.
  • the sleeve 21 Since the sleeve 21 is not subjected to the same stresses as the compressor wheel, it may be manufactured from a material which is much easier to work than the material of the compressor wheel.
  • the relatively small diameter bore required to mount a compressor wheel on to a small diameter shaft can be provided with a high degree of accuracy and manufacturing ease. Since the sleeve 21 fits within the bore 20 in the same manner as would a larger diameter shaft, wheel balancing issues are essentially unchanged. In addition, with the present invention it is not necessary to modify other components of the compressor wheel assembly, such as the wheel clamping arrangement.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Compressor (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP03256589A 2002-10-24 2003-10-20 Assemblage de roue de compresseur Withdrawn EP1413767A3 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0224723 2002-10-24
GBGB0224723.7A GB0224723D0 (en) 2002-10-24 2002-10-24 Compressor wheel assembly

Publications (2)

Publication Number Publication Date
EP1413767A2 true EP1413767A2 (fr) 2004-04-28
EP1413767A3 EP1413767A3 (fr) 2005-04-13

Family

ID=9946475

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03256589A Withdrawn EP1413767A3 (fr) 2002-10-24 2003-10-20 Assemblage de roue de compresseur

Country Status (6)

Country Link
US (1) US20040126231A1 (fr)
EP (1) EP1413767A3 (fr)
JP (1) JP2004144094A (fr)
KR (1) KR20040036655A (fr)
CN (1) CN1508445A (fr)
GB (1) GB0224723D0 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102639841A (zh) * 2009-12-22 2012-08-15 博格华纳公司 排气涡轮增压器的轴组件
WO2015175214A1 (fr) 2014-05-12 2015-11-19 Borgwarner Inc. Roue de compresseur comportant un manchon en titane

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0224727D0 (en) * 2002-10-24 2002-12-04 Holset Engineering Co Compressor wheel assembly
GB0224726D0 (en) * 2002-10-24 2002-12-04 Holset Engineering Co Compressor wheel assembly
GB0224721D0 (en) * 2002-10-24 2002-12-04 Holset Engineering Co Compressor wheel assembly
JP4053563B2 (ja) * 2005-12-01 2008-02-27 ファナック株式会社 流体機械
DE602006020239D1 (de) 2006-01-24 2011-04-07 Ihi Corp Motorbetriebene Aufladung
EP1813782B1 (fr) 2006-01-26 2009-08-05 IHI Corporation Turbo-Surpresseur
WO2007108234A1 (fr) * 2006-03-23 2007-09-27 Ihi Corporation Arbre à haute vitesse de rotation pour compresseur
JP4753033B2 (ja) 2006-06-02 2011-08-17 株式会社Ｉｈｉ 電動過給機
CN101506489B (zh) 2006-08-18 2011-11-16 株式会社Ihi 电动增压器
JP4826417B2 (ja) * 2006-09-29 2011-11-30 株式会社ジェイテクト 過給器
DE102007012641A1 (de) * 2007-03-16 2008-09-18 Daimler Ag Laufzeug für einen Abgasturbolader
US8794905B2 (en) * 2008-04-08 2014-08-05 Ihi Corporation Turbocharger
DE102012111154A1 (de) * 2011-11-21 2013-05-23 Ecomotors International, Inc. Bimetallisches Verdichterrad und Verfahren zu dessen Herstellung
KR101912799B1 (ko) * 2012-04-16 2018-10-29 한화파워시스템 주식회사 압축기용 오일 실
JP7166048B2 (ja) * 2017-04-18 2022-11-07 株式会社荏原製作所 中間部材、ポンプ、及びポンプのメンテナンス方法
CN110529324B (zh) * 2019-09-05 2020-10-02 江西理工大学 立式斜击式双喷嘴整装机
CN114704499A (zh) * 2022-04-24 2022-07-05 珠海格力电器股份有限公司 一种转子组件和空气循环机

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2799445A (en) * 1955-12-12 1957-07-16 Gen Electric High speed rotor
US3019039A (en) * 1956-04-09 1962-01-30 Fairchild Stratos Corp Means for mounting a body on a rotating shaft
DE2621201C3 (de) * 1976-05-13 1979-09-27 Maschinenfabrik Augsburg-Nuernberg Ag, 8900 Augsburg Laufrad für eine Strömungsmaschine
US4705463A (en) * 1983-04-21 1987-11-10 The Garrett Corporation Compressor wheel assembly for turbochargers
US5163816A (en) * 1991-07-12 1992-11-17 General Motors Corporation Wheel lock, centering and drive means and turbocharger impeller combination
JP3777648B2 (ja) * 1996-04-03 2006-05-24 石川島播磨重工業株式会社 羽根車の締結構造
DE19736333C1 (de) * 1997-08-21 1999-03-04 Man B & W Diesel Ag Befestigung eines Laufrades einer Strömungsmaschine an einer Welle
US6164931A (en) * 1999-12-15 2000-12-26 Caterpillar Inc. Compressor wheel assembly for turbochargers
US6481970B2 (en) * 2000-06-28 2002-11-19 Honeywell International Inc. Compressor wheel with prestressed hub and interference fit insert
DE10101165C2 (de) * 2001-01-12 2003-06-05 Man B & W Diesel Ag Befestigungsvorrichtung für ein radial durchströmtes Verdichterrad
GB0224726D0 (en) * 2002-10-24 2002-12-04 Holset Engineering Co Compressor wheel assembly
GB0224721D0 (en) * 2002-10-24 2002-12-04 Holset Engineering Co Compressor wheel assembly
GB0224727D0 (en) * 2002-10-24 2002-12-04 Holset Engineering Co Compressor wheel assembly

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102639841A (zh) * 2009-12-22 2012-08-15 博格华纳公司 排气涡轮增压器的轴组件
CN102639841B (zh) * 2009-12-22 2014-07-09 博格华纳公司 排气涡轮增压器的轴组件
WO2015175214A1 (fr) 2014-05-12 2015-11-19 Borgwarner Inc. Roue de compresseur comportant un manchon en titane

Also Published As

Publication number Publication date
CN1508445A (zh) 2004-06-30
GB0224723D0 (en) 2002-12-04
EP1413767A3 (fr) 2005-04-13
JP2004144094A (ja) 2004-05-20
KR20040036655A (ko) 2004-04-30
US20040126231A1 (en) 2004-07-01

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